Aerodynamic effects of leading edge (LE) slats and slotted trailing edge (TE) flaps on NACA-2412 airfoil in prospect of optimization-Reference-Cited by-同舟云学术

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Aerodynamic effects of leading edge (LE) slats and slotted trailing edge (TE) flaps on NACA-2412 airfoil in prospect of optimization

Published:2021 Issue: Volume:44 Page:587-595
ISSN:2214-7853
Container-title:Materials Today: Proceedings
language:en
Short-container-title:Materials Today: Proceedings

Author:

Arra Aditya,Anekar Nitinkumar,Nimbalkar Shrikant

Publisher

Elsevier BV

Subject

General Medicine

Reference17 articles.

1. The aerodynamic design of multi-element high-lift systems for transport airplanes;van Dam;Prog. Aerosp. Sci.,2002

2. Aerodynamic design of high-lift devices for civil transport aircraft using RANS CFD;Schindler;AIAA 2010-4946,2010

3. Optimization of high lift device system deployment for takeoff performance;Giacomelli;18th AIAA/ISSMO Multidiscip. Anal. Optim. Conf. 2017,2017

4. Commercial Airplane Design Principles;Sforza,2014

5. General aviation aircraft design: applied methods and procedures;Gudmundsson,2014

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4. Design of a Novel Aerofoil of a Light Aircraft for Robust Aerodynamic Performance at High Reynolds Number Regime Using XFLR5;Arabian Journal for Science and Engineering;2024-02-26

5. Aerodynamic characteristic of wind turbine with the leading edge slat and Microtab;Sustainable Energy Technologies and Assessments;2022-08

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